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RF Transceiver Module DesignChapter 8
Frequency Synthesis and Phase-Locked Loops
李健榮助理教授
Department of Electronic EngineeringNational Taipei University of Technology
Outline
• Frequency Synthesis Techniques
• Frequency Synthesizers based on the Phase-Locked-Loop
• Loop Analysis and Stability
• Settling Time
• Loop Filters
• Noise Analysis
• PLL Architectures
• Summary
2/55 Department of Electronic Engineering, NTUT
Generic Transceiver Front End
• Local oscillator (LO) provides the carrier signal for both thereceive and transmit paths.
• If the LO output contains phase noise, both downconvertedand upconverted signals are corrupted.
BPFLNA
Duplexer
Antenna
vFrequency Synthesizer LO
PABPF
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Effect of Phase Noise in Receivers
f0f
Wanted Signal
LO Output
Wanted Signal
DownconvertedSignal
f
DownconvertedSignals
ff0f
Wanted Signal
LO Output Interferer
• Reciprocal mixing
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Effect of Phase Noise in Transmitters
f1f
Wanted Signal
Nearby Transmitter
2f
f0f
Multi-carrier signal (or OFDM)
f0f
• Receiver desensitization
• Orthogonality
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• Meaning of frequency
• Meaning of frequency synthesisGeneration of a frequency or frequencies that are exact multiples of a referencefrequency. Usually the reference is very precise and the synthesized frequencies areselectable over some range of whole-number multiples of a submultiple of .
Frequency Synthesis
out ref
nf f
M=
wheren andM are integers,n varies fromNmin to Nmax, andM is constant.
( )v t
t
1T
1
1
f
( )V f
f1f
reff
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Transformation To and From Voltage or Current
A B1f
Frequency Discriminator
∫
C D
d
dt
Voltage Controlled Oscillator (VCO)
Phase Detector Phase Modulator
1 1v Af=2 1f Bv=
1 1f dtφ = ∫ 2 1v Cφ= 2 2Dvφ =
3 2
df
dtφ=
V/Hz Hz/V
V/rad or V/cycle rad/V or cycle/V
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Demonstration of the Transfer Functions
rms rms rms rms rms
1 rad 2 V rad rad 11 V 2 V 2 V V 0.32 V
V cycle cycle 2 radAVπ π
= ⋅ = = = =
RMS voltage at point A:
1 rms
MHz0.32 V 1.5 0.48 MHz
Vf∆ = ⋅ = rms
2
0.32 V MHz1 0.32 MHz
1 k mAf∆ = ⋅ =
Ω( ) rms
5 V0.48 MHz-0.32 MHz 0.8 V
MHzDV = ⋅ =
Phase Modulator1 rad/V
Phase Detector2 V/Cycle
220 MHz VCO1.5 MHz/V
1 kΩ
200 MHz ICO1 MHz/mA
100 MHz signal
Low-pass Filter
50 MHz Cut-off
Frequency Discriminator
5 V/MHz
AB
DModulation voltage(1 Vrms at 10 kHz)
C
and
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• Frequency addition and subtraction:
Mathematical Operations on Frequency
( ) ( )cos 2RF RF RFv t A f tπ θ= +
( ) ( ) ( ) ( ) ( )cos 2 cos 2IF RF LO RF RF LO LOv t v t v t A f t B f tπ θ π θ= ⋅ = + × +
For the practical mixer with nonlinear operation:
IF RF LOf mf nf= +
( ) ( )cos 2LO LO LOv t B f tπ θ= +
( ) ( ) ( ) ( ) cos 2 cos 22 RF LO RF LO RF LO RF LO
ABf f t f f tπ θ θ π θ θ= + + + + − + −
( ) ( ) ( )cos 2 cos 2 for 02 RF LO RF LO RF LO
ABf f t f f tπ π θ θ= + + − = =
( ) ( ), cosIF m nv t K m nα β= + 2 1f Bv= 2 LO LOf tβ π θ= +where and
or we can say the intermediate frequency is:
RF
LO
IF
Mixer
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Frequency Synthesis Techniques
• Direct Analog Synthesis (DAS)
• Direct Digital Synthesis (DDS)
• Indirect Synthesis : Phase-Locked Loops (PLLs)
• Hybrid DDS/PLL
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• Frequency generated by mixed frequencies
Direct Analog Synthesis (DAS) (I)
1f
2f
3f
2Nf −
1Nf −
Nf
outf
filter1
filter2
filter3
filterN-2
filterN-1
filterN
out a bf mf nf= ±
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• More stages are required for flexibly frequency planning.
Direct Analog Synthesis (DAS) (II)
1f
2f
3f
2Nf −
1Nf −
Nf
filter1
filter2
filter3
filterN-2
filterN-1
filterN
filter1
filter2
filter3
filterN-2
filterN-1
filterN
outf
1f ′ 2f ′3f ′ 2Nf −′ 1Nf −′ Nf ′
( )out a b cf p mf nf qf= ± ±
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Direct Digital Synthesis (DDS) (I)
ref cf f=
• Waveform construction is based on the lookup table (LUT)and a digital to analog converter (DAC).
• Direct synthesis
• Generated frequency is lower than input frequency
Ref. Clk
PhaseAccumulator
Amplitude/SinConv. Algorithm
DACTuning word
N
Digital Analog
2o cN
Mf f= ⋅
M
Jump size
0000…0
1111…1
1111…0
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Direct Digital Synthesis (DDS) (II)
• Hardware technique to reduce the spur level of a DDS
• Reduce bandwidth
1000 MHz
100−150 MHz 1100−1150 MHz 110−115 MHz
div-by-10
DDS FilterFrequency
Divider
0f
outf
BW=50 MHz BW=15 MHz
reff
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Hybrid DDS/DAS
1f ′ 2f ′ 3f ′2Nf −′ 1Nf −′ Nf ′
outf
filter1
filter2
filter3
filterN-2
filterN-1
filterN
DDS FrequencyDivider
reff
• Scheme to increase a DDS output bandwidth
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• The main goal of the PLL is to sync the divided oscillatorfrequency with the reference frequency .
Indirect Frequency Synthesis
( )outf N reff
( )out reff N f= out reff N f= ⋅
PFD: Phase frequency detector LPF: Loop filter VCO: Voltage controlled oscillator /N: Divided-by-N frequency divider
Frequency divider
reffoutf
/N
PFD LPF
VCO
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Fractional-N Frequency Synthesis
• Lower division ratioN to reduce inband phase-noise gain
• Effectively produce a fractional division value
• Generally employee a delta-sigma modulator for division ratiodithering
PFD LPF
Dual-modulusFrequency Divider
reff outf
/N, (N+1)
FCW
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Feedback System
( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( ) ( )o i o i oV s V s V s H s G s G s V s V s G s H s= − = −
( )( ) ( ) ( )
( ) ( )1o
i
V s G sT s
V s G s H s= =
+
Closed-loop transfer function T(s)
G(s)H(s) is the open-loop transfer function
( )iV s ( )oV s( )G s
( )H s
error
• Feedback loop:
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Loop Analysis – Use Frequency as I/O
( ) ( )pv
KG s F s K
s=
( ) 1H s
N=
( )( )
( )( ) ( )
( )
( )111
pv
out
prefv
KF s Kf s G s s
Kf s G s H sF s K
N s
= =+ +
• Relation between input and output frequencies:
Phase differenceFrequency difference
Frequency Divider
( )reff s ( )outf s1
spK
vK
1
N
( )outf s
N
PFDLPF VCO
( )F s
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• Relation between input and output phases:
Loop Analysis – Use Phase as I/O
( ) ( ) vp
KG s K F s
s=
( ) 1H s
N=
( )( )
( )( ) ( )
( )
( )11 1
vp
out
vrefp
KK F ss G s s
Ks G s H s K F sN s
φφ
= =+ +
Frequency Divider
( )ref sφ ( )out sφpK ( )F s
vK
s
1
N
Phase difference Frequency to Phase
PFDLPF VCO
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Loop Transfer Functions
( ) ( )( )
( )( )
( )( ) ( )
0 0
0 01 1p po
i p p
K F s K s K F s K G sT s
K F s K Ns Ns K F s K G s H s
φφ
= = = =+ + +
T(s) : closed-loop PLL transfer function
G(s) : forward-path transfer function
F(s) : loop filter transfer function
Kp: phase detector gain
K0/s: VCO transfer function
( ) ( )1 0G s H s+ = ( ) ( ) 1 0 dB@ 180G s H s = − = ∠ −
H(s) : feedback-path transfer function
G(s)H(s) : open-loop transfer function
or
• A PLL is unstable when
The condition of unity open loop gain and a phase angle of 180 degrees must be avoided.
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PLL Response w/o a Loop Filter (I)
( ) 0 0
0 01
Fp LPFo
Fi p LPF
KK K K s NT s N N
KK K K Ns ss N
φ ωφ ω
= = = =+ ++
( ) LPFF s K=
0ω
logω
dB
0FK
Nω ω= =
20 logN
3 dB
0ω
• Closed-loop transfer function:
Without the loop filter, the feedback loop is equivalent to a DC gain of N plus a low-pass filter (in dB) with cutoff at .
3 dB cutoff frequency is KF/N = KpKLPFK0/N .
With
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• The simplest PLL is called a type-I loop because the open-loopgain has one pole at DC (pure integration). It is also a first-order loop because the open-loop gain has one significant pole:
• The open loop gain has a slope of−6 dB/octave or−20dB/decade for all frequencies.
• The phase angle is always−90 degrees at all frequencies.Hence with no low-pass filter, the PLL is always stable. But themain drawback is that designers loose control over the loop.
PLL Response w/o a Loop Filter (II)
( ) ( ) ( )p vK F s KG s H s
Ns=
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• The function of the LPF is to filter out any high frequencyharmonics in the loop.
• Adding a LPF also affects the loop response includingparameters such as the loop time response, bandwidth, and thedamping factor.
• If we add a low-pass filter with a pole located at , the loopwill be still type-I, but it will become a second-order loop.
Single Pole Loop Filter
( ) ( )1LPF
p
KF s
s ω=
+( ) ( )
1 1
p LPF v F
p p
K K K KN NG s H s
s ss s
ω ω
= =
+ +
pω
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Bode Plot of Open-Loop Transfer Function
( ) ( ) ( )1
G sG s H s
N= = ( )G s N= (forward-loop gain )
log mω
( ) ( )m mG Hω ω
6 dB/oct−1020log FK
N
0 dB
Lωpω1mω =
90−
135−
180−
( )mG ω∠
12 dB/oct−
Phase margin
• Where the curves cross, the open-loop gain equals unity.
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• Prototype 2nd-order equation:
• Natural frequency:
• Damping ratio:
Natural Frequency and Damping Ratio
( ) ( )( ) ( )
( )( )
0
0
1
1 1 1 11
F
ppo F
Fi pF
p
p
K
ssK F s K sG s NK
T sKG s H s K F s K Ns sNs KsNs
ωφφ
ωω
+ = = = = =
+ + + + + +
0F p
n p
K
N
ωω ω ω= =
0
1 1 1
2 2 2p p
pn F
N
K
ω ως ω
ω ω= = =
It is geometric mean of the loop bandwidth in the absence of a filter and the filtercorner frequency.
2
2 2 2 22 2 2
p F p F n
p F n n n np
K KN
K s s s ss s
N
ω ω ωω ςω ω ςω ωω
= = =+ + + ++ + Characteristics equation
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• The poles of the closed-loop function:
• As long as damping ratio is greater than one, the poles are realand a tangential plot of closed loop gain looks like:
Closed-Loop Gain for Large Damping
20logN
6 dB/oct−
12 dB/oct−
log mω
( )out
ref
fs
f
2 202 1 1 1ω ω ς ς = − −
21 1 1
2pω
ω ς = + −
The characteristics are similar to the case with no loop filter, except for theincreasing rate of attenuation in fout/fref beyond approximately the filter cornerfrequency .
2 1p n ns ςω ω ς= − ± −
0ω
pω
pωDepartment of Electronic Engineering, NTUT28/55
• As decreases toward , the damping ratio decreases andthe phase shift at increases. Correspondingly, the transientresponse of the loop becomes less damped (more ringing) andthe response peaks near .
Close-Loop Responses
0F p
n p
K
N
ωω ω ω= =
0
1 1 1
2 2 2p p
pn F
N
K
ω ως ω
ω ω= = =
pω 0ω0ω
nω
m nω ω0.25 0.5 1 2 4
12 dB
6 dB
0 dB
−6 dB
−12 dB
−18 dB
−24 dB
0.1ς =0.3
0.50.7
1 ( )1 out
ref
f
N fω
0mω ω
0.1ς =12 dB
6 dB
0 dB
−6 dB
−12 dB
−18 dB
−24 dB
−30 dB
0.25 0.5 1 2 4
( )1 out
ref
f
N fω
0.3
2
0.5 0.71
Tangent for no filter
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Relative Stability – Phase Margin
• Right figure shows the phase margin(relative stability) as a function of thedamping factor. More highly dampedloops are safer, in that more parametervariation is allowable before instabilityoccurs.
log mω
( ) ( )m mG Hω ω
6 dB/oct−1020log FK
N
0 dB
Lωpω1mω =
90−
135−
180−
( )mG ω∠
12 dB/oct−
Phase margin
• With a single-pole low-pass filter, theloop is inherently stable, sine−180o
phase shift cannot be attained for anyfinite frequency.(not always true practically)
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ς0.2 0.3 0.5 0.7 1.0 2.00.1
10
20
30
40
50
60
70
80
0
90
14
1 190 tan 1 1
2 4PM
ς−
= − + −
Pha
se M
arg
in (
degr
ee
s)
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Transient Response
0t = t
oldf
newf
Synthesizer output frequency
A
B
CD
Overshot
Ringing• Lower damping ratio brings
a higher percent overshootcan cause the loop to go outof lock. (more unstable)
• Narrower bandwidth withsmaller damping ratio andlonger settling time.
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1N
2N
1 refN f
2 refN f
( )2 1N N>
e
1
2
1 ref
Nf
N
−
t
reff outf( )G s
1 N
e
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Settling Time
( )( )0
02.3log
fT
f Tω∆∆
≃
oldf
newf( )0f∆
0t = t T=
( )f T∆
3 -11 MHz/cycle 10 secFK = =10 kHzreff =
11 MHz 10 MHzoutf = →
Find the settling time for the output frequency of 10.1 MHz is attained:6
0
101000
1000FK
Nω = = =
0
2.3 1log 2.3 ms
0.1T
ω=≃
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• Settling time:The frequency error changes one decade approximately each 2.3 time constant, i.e.,
• Example (no filter):
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• The addition of a pole in the transfer function causes theslope to drop at a rate of−6 dB/oct whereas the addition of azero has the opposite effect.
• The open loop transfer function is:
• The closed-loop transfer function is:
A Pole-Zero Filter
( ) ( )( )
1
1z
p
sF s
s
ωω
+=
+
( ) ( ) ( ) ( )( )
1
1
p v zp v
p
K K sK F s KG s H s
Ns Ns s
ωω
+ = = +
pω
zω
6 dB/oct−
12 dB/oct−
log mωzωpω
6 dB/oct−
( ) ( )( )
0
01po
i p
K F s K sT s
K F s K Ns
θθ
= =+
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Open-Loop Gain with a Pole-Zero LPF (I)
( )( )
2
1
1
p Fz
p F p Fp
z
Ks
NT s NK K
s sN N
ωω
ω ωω
ω
+=
+ + +
0F
n p p
K
Nω ω ω ω= =
1
2p n
n z
ω ωςω ω
= +
6 dB/oct−
12 dB/oct−
log mωzωpω
6 dB/oct−
( )22 2
1
2z
nn n
sN
s s
ωω
ςω ω+
=+ +
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• Given the pole frequency location, a zero can be placed afterthe so as to avoid the magnitude fromcrossing the unity gainaxis at a slope of−12 dB/oct, and therefore avoiding instability.To determine the closed loop response, simply plotT(s):
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• Fromthe results:
Selecting the pole frequency sets the natural frequency and subsequently theloop bandwidth.
Selecting the zero (based on the pole location in the open loop gain response)determines the desired percentage overshoot.
• Therefore, a pole-zero filter allows the designer to select theloop bandwidth and the damping factor independently and stillachieve stability.
Open-Loop Gain with a Pole-Zero LPF (II)
0F
n p p
K
Nω ω ω ω= =
1
2p n
n z
ω ωςω ω
= +
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• The simplest PLL is the type-I loop because the open-loop gainhas one pole at DC (pure integration). It is also a first-orderloop because the open-loop gain has one significant pole.
Type and Order of the Loop
( ) ( )( ) ( )
( )( )1
G s N sT s
G s H s D s= =
+
( ) 11 0
n nn nN s a s a s a−
−= + + +⋯
( ) 11 0
m mm mD s b s b s b−
−= + + +⋯Order = m (m roots)Type = n (n roots at DC)
( )ref sφ ( )out sφpK ( )F s
vK
s
1
N
PFDLPF VCO
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• First order, type I (no loop filter)
First-order Type I
Lωlog mω0 dB
G
6 dB/oct.−
1Riv ov
2R
2
1 2
oLPF
i
v RG
v R R= =
+
A−3R
iv
4R
ov′A → ∞
4
3
oLPF
i
v RG
v R
′′− = = −
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• Second order, type I (lag-and-lead filter)
Second-order Type I (I)
1Riv
ov
2R
1C
A−3R
iv5R
ov
2C
4R
Lωlog mω0 dB
G
12 dB/oct.−
6 dB/oct.−zωpω
1
1
zLPF
p
s
Gs
ω
ω
+=
+
2 1
1z R C
ω =( )1 2 1
1p R R C
ω =+
1
1
zLPF
p
s
Gs
ω
ω
+′′− =
+′
4 52
4 5
1z R R
CR R
ω′ =
+5 2
1p R C
ω′ =
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• Second order, type I (lag filter)
Second-order Type I (II)
Lωlog mω0 dB
G
6 dB/oct.−
pω
12 dB/oct.−
2
1 2
1
1LPF
p
RG
sR Rω
−=+ +
4
3
1
1LPF
p
RG
sRω
′− = −+
′1 1 2
1 1 1p C R R
ω = +
4 2
1p R C
ω′ =
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1Riv
ov
2R 1C
A−3R 4R
ov′
2C
A → ∞iv
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• Second order, type II (integrator and lead filter)
Second-order Type II
Lωlog mω0 dB
G12 dB/oct.−
6 dB/oct.−zω
1 1
11 z
LPF
s
GR C s
ω+
− = −
2
1z R C
ω =
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A−1R
iv
2R
ov
C
A → ∞
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• Third order, type II (integrator plus lead-lag filter)
Third-order Type II
Lωlog mω0 dB
G
12 dB/oct.−
pω
12 dB/oct.−6 dB/oct.−
zω
1 1
11
1
zLPF
p
s
GR C s
s
ω
ω
+− = −
+
3 3
11
1
zLPF
p
s
GR C s
s
ω
ω
+′′− = −
+ ′
( )2 1 2
1z R C C
ω =+ 2 2
1p R C
ω =4 3
1z R C
ω′ =5 4
1p R C
ω′ =
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A−1R
iv2R
ov
2C
1C
A → ∞
A−3R
iv
4R
ov′
3C
5R
4CA → ∞
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PLL Phase Noise Model
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Frequency Divider
Xtal
,ref nφ
outφ
1
N
PFD LPF
,pfd nV ,op nV ,vco nφ
,div nφ
VCO
+ ++ +
+
( ) ( ) ( ) ( ) ( ), , , , , ,out n pfd n op n ref n div n e vco nd
T sV V T s H s
Kφ φ φ φ= + + + +
( ) ( )( ) ( )1
G sT s
G s H s=
+
( ) ( ) ( )1
1eH sG s H s
=+
( ) ( )( ) ( ) ( )
for
for1c
c
NG sT s
G sG s H s
ω ωω ω
<<= ≈ >>+
( ) ( ) ( )( ) for 1
for11
ce
c
N
G sH sG s H s
ω ωω ω
<<= ≈ >>+
where
Very useful results
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Responses of Noise Transfer Functions
cωlog mω
( )( ) ( )1
G s
G s H s+N
( )G s
Transfer function multiplyingall sources except VCO
cωlog mω
( ) ( )1
1 G s H s+1
( ) ( )1
G s H s
Transfer function for VCO
cω log mω
20logN
( )dB
0
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Other sources dominateinband noise
VCO dominatesoutband noise
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Typical VCO and PLL Noise Performance
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( )L f∆(dBc/Hz)
VCOPLL
( )log f∆1 kHz 10 kHz 100 kHz 1 MHz 10 MHz
−120
−90
−60−30 dB/dec
−20 dB/dec
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Phase-Locked Loop Architectures
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• Integer-N PLL• Offset PLL• Fractional-N PLL• DDS offset PLL• Dual loop PLL• Multi-loop PLL
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• Lower division ratio N to reduce inband phase-noise gain• Extend bandwidth with different • Avoid LO pulling
Offset PLL
out ref offsetf N f f= ⋅ +
offsetf
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PFD LPF
Frequency Divider
reff outf
/N
offsetf ?
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Offset PLL − Dual-Loop PLL (I)
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PFD LPF
Frequency Divider
reff outf
/N
PFD LPF
Frequency Divider
offsetf
/M
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Offset PLL − Dual-Loop PLL (II)
PFD LPF
Frequency Divider
1reff outf
/N
PFD LPF
Frequency Divider
offsetf
/M
2reff
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Offset PLL − Hybrid DDS/PLL
PFD LPF
Frequency Divider
reff outf
/N
DDS
offsetf
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Multi-Loop PLL
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PFD LPF
Frequency Divider
reff outf
/N
1offsetf
PFD LPF
/M
PFD LPF
/P
2offsetf
3offsetf
50/55
• Lower division ratio N to reduce inband phase-noise gain• Effectively produce a fractional division value• Generally employee a delta-sigma modulator for division ratio
dithering
Fractional-N Frequency Synthesis
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PFD LPF
Dual-modulusFrequency Divider
reff outf
/N, (N+1)
FCW
51/55
• DDS acts a reference source or phase/frequency modulator• A variable reference frequency source can drive a fractional
frequency output.
DDS-Driven Fractional-N Synthesizer
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PFD LPF
Frequency Divider
reff outf
/N
Hybrid DDS/PLL
FCW
DDS
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DDS-feedback Fractional-N Synthesizer
2out ref offsetn
Mf f f= ⋅ +
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PFD LPF
DDS as aFrequency Divider
reff outf
DDS
FCW
Hybrid DDS/PLL
• DDS acts a frequency divider
• DDS output frequency:
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Comparison of Frequency Synthesizers
DDSSingle-Loop
PLLMulti-Loop
PLLDDS/DAS
DDS OffsetPLL
DDS DrivenPLL
BW(output)
Narrow
< 100MHz
Broad
> 1GHz
Broad
> 1GHz
Broad
> DDS
Broad
(carefully design)
Broad
ResolutionExtremely
Fine
< 0.02 Hz
Very Course
> 250kHz
(typical)
Medium
> 1kHz
(typical)
Extremely Fine
< 0.01 Hz
Extremely Fine
< 0.01 Hz
Extremely Fine
< 1Hz
SwitchingTime
Very Fast
< 100 ns
Fast
< 100us
(typical)
Very Slow
> 1ms
(typical)
Very Fast
< 1us
(limited by RF switch)
Fast
< 100us
(typical)
Trade-off vsclose-in spurious
tones
SpuriousNoise
< 75dBc
(limited by DAC)
Very GoodGood
(carefully design)
Minimum Close-in Spurious
Minimum Close-in Spurious
Excellent over Broad Bandwidth
PhaseNoise
Better than clock
referenceVery Good Very Good Very Good Very Good Good
Circuitry Simple Simple Very Complex Moderate Moderate Moderate
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Summary
• In this chapter, the basic idea of the phase-locked loopsderived fromthe feedback systemwas introduced. One mayput attention on that the PLL is processing the phase (orfrequency) by transforming the phase error into voltage orcurrent signals.
• The PLL transient response and the phase noise were alsopresented in this chapter. We can simply conclude that, as loopbandwidth increases, the locking time is going faster and theVCO inband phase noise can be suppressed with moreattenuation while the other components contribute more noisewithin the loop bandwidth.
Department of Electronic Engineering, NTUT55/55